An aircraft propeller blade is constructed by forming two shells of composite material laminates and bonding the two shells to a metallic spar with foam filler pieces interposed between the shells at desired locations. The blade is then balanced radially and chordwise.


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    Titel :

    Method of making counterrotating aircraft propeller blades


    Beteiligte:

    Erscheinungsdatum :

    1990-11-20


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Counterrotating aircraft propulsor blades

    Nelson, Joey L. / Elston, III, Sidney B. / Tseng, Wu-Yang et al. | NTRS | 1988


    Counterrotating aircraft propulsor blades

    Nelson, Joey L. / Elston, III, Sidney B. / Tseng, Wu-Yang et al. | NTRS | 1993



    Performance and Acoustic Prediction of Counterrotating Propeller Configurations

    Denner, B.W. / Korkan, K.D. | SAE Technical Papers | 1989